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FR3088980B1 - LUBRICATION AND COOLING CORE FOR AN AIRCRAFT TURBOMACHINE MECHANICAL REDUCER - Google Patents

LUBRICATION AND COOLING CORE FOR AN AIRCRAFT TURBOMACHINE MECHANICAL REDUCER Download PDF

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Publication number
FR3088980B1
FR3088980B1 FR1871749A FR1871749A FR3088980B1 FR 3088980 B1 FR3088980 B1 FR 3088980B1 FR 1871749 A FR1871749 A FR 1871749A FR 1871749 A FR1871749 A FR 1871749A FR 3088980 B1 FR3088980 B1 FR 3088980B1
Authority
FR
France
Prior art keywords
axis
lubrication
flanges
cooling core
aircraft turbomachine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR1871749A
Other languages
French (fr)
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FR3088980A1 (en
Inventor
Adrien Louis Simon
Giovanni Jean-Charles Michel Pierre Di
Boris Pierre Marcel Morelli
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Transmission Systems SAS
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Safran Transmission Systems SAS
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Filing date
Publication date
Application filed by Safran Transmission Systems SAS filed Critical Safran Transmission Systems SAS
Priority to FR1871749A priority Critical patent/FR3088980B1/en
Priority to EP19209234.4A priority patent/EP3657044B1/en
Priority to US16/691,412 priority patent/US11339869B2/en
Priority to CN201911155371.6A priority patent/CN111219255B/en
Publication of FR3088980A1 publication Critical patent/FR3088980A1/en
Application granted granted Critical
Publication of FR3088980B1 publication Critical patent/FR3088980B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/04—Features relating to lubrication or cooling or heating
    • F16H57/0467—Elements of gearings to be lubricated, cooled or heated
    • F16H57/0479—Gears or bearings on planet carriers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/04—Features relating to lubrication or cooling or heating
    • F16H57/042—Guidance of lubricant
    • F16H57/0427—Guidance of lubricant on rotary parts, e.g. using baffles for collecting lubricant by centrifugal force
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/06—Arrangements of bearings; Lubricating
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/04—Features relating to lubrication or cooling or heating
    • F16H57/0412—Cooling or heating; Control of temperature
    • F16H57/0415—Air cooling or ventilation; Heat exchangers; Thermal insulations
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/04—Features relating to lubrication or cooling or heating
    • F16H57/042—Guidance of lubricant
    • F16H57/043—Guidance of lubricant within rotary parts, e.g. axial channels or radial openings in shafts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/04—Features relating to lubrication or cooling or heating
    • F16H57/0434—Features relating to lubrication or cooling or heating relating to lubrication supply, e.g. pumps ; Pressure control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/04—Features relating to lubrication or cooling or heating
    • F16H57/0456—Lubrication by injection; Injection nozzles or tubes therefor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/04—Features relating to lubrication or cooling or heating
    • F16H57/0467—Elements of gearings to be lubricated, cooled or heated
    • F16H57/0469—Bearings or seals
    • F16H57/0471—Bearing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/04—Features relating to lubrication or cooling or heating
    • F16H57/048—Type of gearings to be lubricated, cooled or heated
    • F16H57/0482—Gearings with gears having orbital motion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/04—Features relating to lubrication or cooling or heating
    • F16H57/048—Type of gearings to be lubricated, cooled or heated
    • F16H57/0482—Gearings with gears having orbital motion
    • F16H57/0486—Gearings with gears having orbital motion with fixed gear ratio
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/08—General details of gearing of gearings with members having orbital motion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/98—Lubrication
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H1/00—Toothed gearings for conveying rotary motion
    • F16H1/28—Toothed gearings for conveying rotary motion with gears having orbital motion
    • F16H1/36—Toothed gearings for conveying rotary motion with gears having orbital motion with two central gears coupled by intermeshing orbital gears
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/08—General details of gearing of gearings with members having orbital motion
    • F16H2057/085—Bearings for orbital gears

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Details Of Gearings (AREA)
  • Retarders (AREA)

Abstract

Noyau (22) de lubrification et de refroidissement pour un réducteur mécanique de turbomachine, en particulier d’aéronef, caractérisé en ce qu’il est destiné à être monté dans un axe (10b) d’un satellite dudit réducteur, et comprend des premier et second flasques (22a, 22b) coaxiaux et sensiblement tronconiques comportant chacun une première extrémité de plus grand diamètre et une seconde extrémité opposée de plus petit diamètre, les flasques étant fixés ensemble par leurs secondes extrémités et étant destinés à s’étendre à l’intérieur dudit axe et à recouvrir au moins une surface radialement interne (10e, 10f) de cet axe pour définir avec celle-ci au moins une cavité annulaire (24) de circulation d’huile de lubrification et de refroidissement de cet axe, lesdites secondes extrémités desdits premier et second flasques comportant des moyens de raccordement fluidique de ladite au moins une cavité à une source d’huile de lubrification et de refroidissement. Figure pour l'abrégé :Figure 8Lubrication and cooling core (22) for a mechanical reduction gear for a turbomachine, in particular an aircraft, characterized in that it is intended to be mounted in an axis (10b) of a satellite of said reduction gear, and comprises first and second coaxial and substantially frustoconical second flanges (22a, 22b) each having a first end of larger diameter and an opposite second end of smaller diameter, the flanges being secured together at their second ends and being intended to extend to the end. interior of said axis and to cover at least one radially internal surface (10e, 10f) of this axis in order to define therewith at least one annular cavity (24) for circulating lubricating and cooling oil of this axis, said seconds ends of said first and second flanges comprising means for fluid connection of said at least one cavity to a source of lubricating and cooling oil. Figure for abstract: Figure 8

FR1871749A 2018-11-23 2018-11-23 LUBRICATION AND COOLING CORE FOR AN AIRCRAFT TURBOMACHINE MECHANICAL REDUCER Active FR3088980B1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1871749A FR3088980B1 (en) 2018-11-23 2018-11-23 LUBRICATION AND COOLING CORE FOR AN AIRCRAFT TURBOMACHINE MECHANICAL REDUCER
EP19209234.4A EP3657044B1 (en) 2018-11-23 2019-11-14 Lubrication and cooling core for a mecanical reducer of a aircraft's turbomachine
US16/691,412 US11339869B2 (en) 2018-11-23 2019-11-21 Lubricating and cooling core for a mechanical reduction gear of an aircraft turbine engine
CN201911155371.6A CN111219255B (en) 2018-11-23 2019-11-22 Lubrication and cooling core for a mechanical speed reducer of a turbine engine of an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1871749A FR3088980B1 (en) 2018-11-23 2018-11-23 LUBRICATION AND COOLING CORE FOR AN AIRCRAFT TURBOMACHINE MECHANICAL REDUCER

Publications (2)

Publication Number Publication Date
FR3088980A1 FR3088980A1 (en) 2020-05-29
FR3088980B1 true FR3088980B1 (en) 2021-01-08

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
FR1871749A Active FR3088980B1 (en) 2018-11-23 2018-11-23 LUBRICATION AND COOLING CORE FOR AN AIRCRAFT TURBOMACHINE MECHANICAL REDUCER

Country Status (4)

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US (1) US11339869B2 (en)
EP (1) EP3657044B1 (en)
CN (1) CN111219255B (en)
FR (1) FR3088980B1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3088977B1 (en) * 2018-11-23 2020-11-27 Safran Trans Systems LUBRICATING OIL DISPENSER FOR AN AIRCRAFT TURBOMACHINE MECHANICAL REDUCER
FR3092889B1 (en) * 2019-02-14 2021-12-03 Safran Trans Systems LUBRICATION OF A SATELLITE CARRIER FOR A MECHANICAL TURBOMACHINE REDUCER, IN PARTICULAR OF AIRCRAFT
US11542842B2 (en) * 2021-05-24 2023-01-03 Borgwarner Inc. Electrically-actuated camshaft phasers with tapered features
CN114877033B (en) * 2022-06-07 2023-09-15 南高齿(淮安)高速齿轮制造有限公司 Transmission mechanism

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1357038A (en) * 1963-02-19 1964-04-03 Rolls Royce Motor driven fan
US3741343A (en) * 1971-04-29 1973-06-26 Clark Equipment Co Lubrication system for a differential
US3893786A (en) * 1973-06-07 1975-07-08 Ford Motor Co Air cooled shroud for a gas turbine engine
US4205525A (en) * 1978-03-17 1980-06-03 Teledyne Industries, Inc. Turbine engine lubrication system
FR2942284B1 (en) 2009-02-16 2011-03-04 Snecma LUBRICATION AND COOLING OF AN EPICYCLOIDAL GEAR TRAIN REDUCER
US8398517B2 (en) * 2009-06-10 2013-03-19 United Technologies Corporation Journal bearing with single unit jumper tube and filter
US9599406B2 (en) * 2010-01-27 2017-03-21 Rexnord Industries, Llc Transmission having a fluid cooling shroud
FR2987416B1 (en) 2012-02-23 2015-09-04 Snecma DEVICE FOR LUBRICATING AN EPICYCLOIDAL REDUCER.
CA2889542A1 (en) * 2014-04-30 2015-10-30 Ge Avio S.R.L. Epyciclic transmission provided with a lubricating system
US9797475B2 (en) * 2014-05-27 2017-10-24 Ge Avio S.R.L. Epicyclic transmission
JP6498559B2 (en) * 2015-07-31 2019-04-10 川崎重工業株式会社 Lubrication structure for planetary gear unit
FR3041054B1 (en) 2015-09-15 2017-09-15 Hispano-Suiza OIL SUPPLY DEVICE FOR AN EPICYCLOIDAL TRAIN REDUCER.
ES2814177T5 (en) * 2016-09-02 2024-06-04 Flender Gmbh planetary gear
DE102017127876A1 (en) * 2017-11-24 2019-05-29 Rolls-Royce Deutschland Ltd & Co Kg Planetary gear and plain bearing pin for a planetary gear
FR3084429B1 (en) * 2018-07-26 2020-11-13 Safran Trans Systems REDUCER OR DIFFERENTIAL TYPE DEVICE FOR AN AIRCRAFT TURBOMACHINE

Also Published As

Publication number Publication date
US11339869B2 (en) 2022-05-24
FR3088980A1 (en) 2020-05-29
EP3657044B1 (en) 2024-02-14
CN111219255A (en) 2020-06-02
EP3657044A1 (en) 2020-05-27
CN111219255B (en) 2024-01-02
US20200166117A1 (en) 2020-05-28

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